Coefficient of Lift Equation with Coefficient of Normal Force Calculator

✖Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow.ⓘ Coefficient of Force [μ]			+10% -10%
✖Angle of attack is the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving.ⓘ Angle of Attack [α]			+10% -10%

✖The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.ⓘ Coefficient of Lift Equation with Coefficient of Normal Force [C_L]

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Coefficient of Lift Equation with Coefficient of Normal Force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Lift Coefficient = Coefficient of Force*cos(Angle of Attack)
C_L = μ*cos(α)
This formula uses 1 Functions, 3 Variables

Functions Used

cos - Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle., cos(Angle)

Variables Used

Lift Coefficient - The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.
Coefficient of Force - Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow.
Angle of Attack - (Measured in Radian) - Angle of attack is the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving.

STEP 1: Convert Input(s) to Base Unit

Coefficient of Force: 0.45 --> No Conversion Required
Angle of Attack: 10.94 Degree --> 0.190939020168144 Radian (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_L = μ*cos(α) --> 0.45*cos(0.190939020168144)

Evaluating ... ...

C_L = 0.441821906948958

STEP 3: Convert Result to Output's Unit

0.441821906948958 --> No Conversion Required

FINAL ANSWER

0.441821906948958 ≈ 0.441822 <-- Lift Coefficient

(Calculation completed in 00.004 seconds)

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Amrita School of Engineering (ASE), Vallikavu

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Coefficient of Lift Equation with Coefficient of Normal Force Formula

LaTeX Go

Lift Coefficient = Coefficient of Force*cos(Angle of Attack)
C_L = μ*cos(α)

What is angle of attack?

In fluid dynamics, angle of attack is the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving

How to Calculate Coefficient of Lift Equation with Coefficient of Normal Force?

Coefficient of Lift Equation with Coefficient of Normal Force calculator uses Lift Coefficient = Coefficient of Force*cos(Angle of Attack) to calculate the Lift Coefficient, The Coefficient of lift equation with coefficient of normal force formula is defined as product of coefficient of normal force acting on the body and cosine angle of attack. Lift Coefficient is denoted by C_L symbol.

How to calculate Coefficient of Lift Equation with Coefficient of Normal Force using this online calculator? To use this online calculator for Coefficient of Lift Equation with Coefficient of Normal Force, enter Coefficient of Force (μ) & Angle of Attack (α) and hit the calculate button. Here is how the Coefficient of Lift Equation with Coefficient of Normal Force calculation can be explained with given input values -> 0.441822 = 0.45*cos(0.190939020168144).

FAQ

What is Coefficient of Lift Equation with Coefficient of Normal Force?

The Coefficient of lift equation with coefficient of normal force formula is defined as product of coefficient of normal force acting on the body and cosine angle of attack and is represented as C_L = μ*cos(α) or Lift Coefficient = Coefficient of Force*cos(Angle of Attack). Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow & Angle of attack is the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving.

How to calculate Coefficient of Lift Equation with Coefficient of Normal Force?

The Coefficient of lift equation with coefficient of normal force formula is defined as product of coefficient of normal force acting on the body and cosine angle of attack is calculated using Lift Coefficient = Coefficient of Force*cos(Angle of Attack). To calculate Coefficient of Lift Equation with Coefficient of Normal Force, you need Coefficient of Force (μ) & Angle of Attack (α). With our tool, you need to enter the respective value for Coefficient of Force & Angle of Attack and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Lift Coefficient?

In this formula, Lift Coefficient uses Coefficient of Force & Angle of Attack. We can use 1 other way(s) to calculate the same, which is/are as follows -

Lift Coefficient = 2*(sin(Angle of Attack))^2*cos(Angle of Attack)

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